Sinapius, M. (1997) Normal Mode Testing by Multi-Axial Base Excitation. In: International Forum on Aeroelasticity and Structural Dynamics, 1997, Volume III, Seiten 209-214. CEAS - International Conference on Aeroelasticity and Structural 17-20 June, 1997, Rome, Italy.
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Kurzfassung
Normal mode testing is commonly performed by multiple point excita- tion. For each normal mode the exciter configuration is adapted in location and magnitude in order to compensate for the internal damping forces of the test structure. An alternative to multiple point excitation is a driven-base test using a multi-axial shaker table. Multi-axis shaker facilities have been developed for structural dynamic qualification. However, they can be used for normal mode testing as well. Then, the overall structure is accelerated in space in order to compensate for the internal damping forces. This requires a suitable combination of all six spatial degrees of freedom of the base excitation. In the case of resonance, the structure responds in quadrature related to the base excitation. If this criterion is fulfilled, the structure vibrates in an eigenmode of vibration in the sense of a single degree of freedom system. The paper summarizes the theoretical background of the test method with particular emphasis on the damping estimation, on the determination of the generalized mass, and on finding a suitanble base axis combination. A suitable test rig for the normal mode testing by base excitation, DLR's multi- axis vibration simualtor MAVIS in Goettingen (FRG) is presented. The test procedure and test data evaluation are elucidated. The application on a test structure characterized by closely-spaced eigenfrequencies is presented. The advantages and disadvantages of normal mode testing by means of base excitation are pointed out.
elib-URL des Eintrags: | https://elib.dlr.de/39816/ | ||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=1997, | ||||||||
Titel: | Normal Mode Testing by Multi-Axial Base Excitation. | ||||||||
Autoren: |
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Datum: | 1997 | ||||||||
Erschienen in: | International Forum on Aeroelasticity and Structural Dynamics, 1997, Volume III | ||||||||
Open Access: | Nein | ||||||||
Gold Open Access: | Nein | ||||||||
In SCOPUS: | Nein | ||||||||
In ISI Web of Science: | Nein | ||||||||
Seitenbereich: | Seiten 209-214 | ||||||||
Name der Reihe: | Volume II | ||||||||
Status: | veröffentlicht | ||||||||
Stichwörter: | experimental modal analysis, multi-axial base excitation, normal mode testing | ||||||||
Veranstaltungstitel: | CEAS - International Conference on Aeroelasticity and Structural 17-20 June, 1997, Rome, Italy | ||||||||
HGF - Forschungsbereich: | NICHT SPEZIFIZIERT | ||||||||
HGF - Programm: | Weltraum (alt) | ||||||||
HGF - Programmthema: | W RP - Raumtransport | ||||||||
DLR - Schwerpunkt: | NICHT SPEZIFIZIERT | ||||||||
DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | NICHT SPEZIFIZIERT | ||||||||
Standort: | Göttingen | ||||||||
Institute & Einrichtungen: | Institut für Aeroelastik | ||||||||
Hinterlegt von: | DLR-Beauftragter, elib | ||||||||
Hinterlegt am: | 02 Apr 2006 | ||||||||
Letzte Änderung: | 27 Apr 2009 10:55 |
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